PROGRAMMED MANEUVER-SPECTRUM FATIGUE TESTS OF AIRCRAFT BEAM SPECIMENS

The bending fatigue properties of a group of 7075-T6 AL ALLOY BEAM SPECIMENS WERE FOUND TO BE SIMILAR TO THOSE OF TYPICAL AIRRAFT STRUCTURES. Test results warrant the following conclusions regarding the constant-load-amplitude fatigue properties of the beam specimens. Static prestressing at 100 pct...

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Hauptverfasser:	MORDFIN,LEONARD, HALSEY,NIXON
Format:	Report
Sprache:	eng
Schlagworte:	AIRCRAFT AIRFRAMES ALUMINUM ALLOYS BEAMS (ELECTROMAGNETIC) BEAMS (STRUCTURAL) DEFORMATION FAILURE (MECHANICS) FATIGUE (MECHANICS) LOADING STRESSES TEST EQUIPMENT TEST METHODS
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